01-196-6024
Fuel Tank Aircraft Baffle
01-196-6025
Fuel Tank Aircraft Baffle
01-196-6026
Fuel Tank Aircraft Baffle
01-196-6032
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7983-1
01-196-6033
Structural Component Air Support
Used on acft model c-18a. nha 69-22323-5
01-196-6035
Structural Component Air Support
Used on acft model c-18a. 14.0 in lg, 2.5 in wd, 0.032 in thk; finish 10.10; commercially pure titanium sheet per mil-t-9046 class 6 annealed; nha 65-2494
01-196-6036
Structural Component Air Support
Used on acft model c-18a. located sta 173.50; nha 65-2494
01-196-6038
Structural Component Air Support
Used on acft model c-18a. c/o 1 bushing, 1 fitting; nha 65-18758-54
01-196-6047
Structural Aircraft Panel
Panel assembly-upper aft mlg fairing; opposite -108a; nha 4F75001, eff on 0082 & up; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane 6 to 8lbs per cubic foot
01-196-6048
Structural Aircraft Panel
Panel assembly-upper aft mlg fairing; opposite -107a; nha 4F75001, eff on 0082 & up; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane 6 to 8lbs per cubic foot
01-196-6049
Structural Aircraft Panel
Used on c-5b aircraft. nha 4F75002, eff on 0082 & up; opposite p/n 4F72627-108a; high temperature, polyurethane 6 to 8 lbs max per cubic foot
01-196-6050
Structural Aircraft Panel
Panel assembly-access, lower aft mlg fairing; nha 4F75002, eff on 0082 & up; opposite -107a; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam high temp, polyurethane 6-8lbs per cubic foot
01-196-6051
Structural Aircraft Panel
Panel assembly-upper fwd mlg fairing; opposite -108a; nha 4F75001, eff on 0082 & up; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane, 6 to 8lbs per cubic foot
01-196-6052
Structural Aircraft Panel
Panel assembly-upper fwd mlg fairing; opposite -107a; nha 4F75001, eff on 0082 & up; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane, 6 to 8lbs per cubic foot
01-196-6062
Aircraft Former
73.000" overall length 17.000" overall width 0.250" material thickness
01-196-6063
Aircraft Former
73.000" overall length 19.000" overall width 0.250" material thickness
01-196-7049
Aircraft Fairing
Used on helicopter,model sh-60b.
01-196-8269
Structural Aircraft Panel
Consist of two fittings; one filler; two ribs; two clips; three doublers; one channel, p/n 123W10204-21
01-196-8481
Structural Component Air Support
01-196-8884
Structural Aircraft Plate
01-196-8885
Structural Component Air Support
Used on acft f-16c/d usaf. umatl spec K21A29T8511; finish A403; heat treat per NDTS1500; 54.8"; nha 16B602-3; effective on 4j 1 on, 4k 1 on, 5c 178, 180, 182, 188, 190, 192, 194, 202, 204, 206, 208, 212, 214, 216, 218, 220, 222, 224, 226, 228 231, 233 on, 5d 31, 33, 35, 39 on
01-196-8886
Structural Component Air Support
Used on acft f-16c/d usaf. matl spec K21A29T8511; finish A403; heat treat per NDTS1500; 11.1 inch stock size; nha 16B600-1; effective on 4j 1 on, 4k 1 on, 5c 178, 180, 182, 188, 190, 192, 194, 202, 204, 206, 208, 212, 214, 216, 218, 220, 222, 224, 226, 228 231, 233 on, 5d 31, 33, 35, 39 on
01-196-8887
Structural Component Air Support
Used on acft model a-10a. c/o fitting p/n 160D712511-14, 13 ea. bushing, radius block p/n 160D712506-1, plate nut p/n MS21069L6, as required rivet
01-196-8897
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-lower aft mlg fairing, fus sta 1675.27 to 1724.00; opposite -U08a; nha 4F75001, eff on 0082 & up; matl - glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam high temp., polyurethane 6-8lbs max per cubic foot
01-196-8898
Structural Aircraft Panel
Panel assembly-lower aft mlg fairing; opposite -107a; nha 4F75001, eff on 0082 & up; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam high temp polyurethane 6-8lbs max per cubic foot
01-196-8899
Structural Aircraft Panel
01-196-8900
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly, access, upper aft main landing gear fairing, fuselage station 1804.000 to 1844.000; used on 4F75002-115a, -111a, -107a, -119a, and -123a
01-196-8901
Structural Aircraft Panel
Panel assembly, access, upper aft main landing gear fairing; used on 4F75002-113a, -109a, -105a, -117a, and -121a
01-196-8902
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly, keel beam closure, main landing gear fairing; used on 4F75001-115a, -119a, -123a
01-196-8903
Structural Aircraft Panel
Panel instl-lower, wing to fus fairing; opposite -108c, eff on 0082 & up; c/o: -109a core, size 1.492X38.000X46.000
01-196-8904
Structural Aircraft Panel
Panel instl-lower, wing to fus fairing; opposite -107c, eff on 0082 & up; c/o: -110a core, size 1.492X38.000X46.000
01-196-8905
Structural Aircraft Panel
Panel assembly-upper fwd mlg fairing; nha 4F75001, eff on 0082 & up; opposite -108a; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam high temp polyurethane 6-8lbs per cubic foot
01-196-8906
Structural Aircraft Panel
Panel assembly-upper fwd mlg fairing; nha 4F75001, eff on 0082 & up; opposite -107a; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam high temp polyurethane 6-8lbs per cubic foot
01-196-8907
Structural Aircraft Panel
Rpanel assembly-lower fwd mlg fairing; opposite -108a, eff on 0082 & up; nha 4F75001; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethan, 6-8lbs per cubic foot
01-196-8908
Structural Aircraft Panel
Panel assembly-lower fwd mlg fairing; opposite -107a, eff on 0082 & up; nha 4F75001; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane, 6-8lbs per cubic foot
01-196-8909
Structural Aircraft Panel
Panel assembly-lower fwd mlg fairing; nha 4F75001, eff on 0082 & up; opposite -108a; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane, 6-8lbs per cubic foot
01-196-8910
Structural Aircraft Panel
Panel assembly-lower fwd mlg fairing; nha 4F75001, eff on 0082 & up; opposite -107a; matl glass fabric per STM22-502 preimpregnated with epoxy resin per mil-r-9300, type i & foam, high temp polyurethane, 6-8lbs per cubic foot
01-196-8918
Aircraft Former
3.900" overall length 2.930" overall width
01-196-8920
Aircraft Former
01-196-8923
Stiffener Aircraft Rib
01-196-9038
Thermal Insulation Pipe Covering
Acft c-130
01-196-9781
Aircraft Engine Build- Parts Kit
01-197-1644
Aircraft Skin
Used on aircraft model f-14.
01-197-1645
Aircraft Skin
Used on aircraft model f-14.
01-197-1646
Aircraft Skin
Used on aircraft model f-14.
01-197-4576
Structural Component Air Support
Aluminu alloy, qq-a-250/11, alloy 6061, T6; 1.335 in. lg, 0.824 in. w, 0.190 in. thk; 2 holes 2-56 unc-2b, 0.640 in. center to center of holes, 0.500 in. from protrusion, 0.092 in. from edge along the length to the cl of holes; 2 holes 0.80 unf-2b x.15 min deep, 0.125 in. from top edge to protrsion bottom, 0.062 in. from cl to the top edge, 0.700 in. from center to center of holes, 0.125 in. protrusion w; 2 holes opposite end 2-56 unc-2b x .21 min deep, 0.640 in. center to center of holes, 0.092 in. from edge od lg, 0.095 in. from edge of bottom
01-197-5394
Aircraft Windshield Panel
01-197-6988
Structural Aircraft Plate
50.000" overall length 3.000" overall width 0.500" material thickness
01-197-6989
Aircraft Fairing
01-197-8632
Structural Aircraft Plate
Al alloy sh, qq-a-250/4, T3, 0.810 in.lg
